DOC AIRBUS | AMM A320FENGINE FUEL AND CONTROL - GENERAL - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The Full Authority Digital Engine Control (FADEC) System has an Electronic Engine Control (EEC) that is designed to be an interface with aircraft displays and computers, control engine fuel flow, and it keeps engine operations stable while in all phases of operation.
The engine fuel and control system supplies calculated fuel flow to the fuel nozzles for combustion, servo fuel pressure for valves and actuators operated by fuel, as well as monitors the system and indicates fault warnings or displays in the cockpit. It also adjusts engine thrust control for stable condition and temporary engine operation as related to applicable systems which include cockpit controls, aircraft configuration information, and aircraft air data.
** ON A/C NOT FOR ALL The Full Authority Digital Engine Control (FADEC) System has an Electronic Engine Control (EEC) that is designed to be an interface with aircraft displays and computers, control engine fuel flow, and it keeps engine operations stable while in all phases of operation.
The engine fuel and control system supplies calculated fuel flow to the fuel nozzles for combustion, servo fuel pressure for valves and actuators operated by fuel, as well as monitors the system and indicates fault warnings or displays in the cockpit. It also adjusts engine thrust control for stable condition and temporary engine operation as related to applicable systems which include cockpit controls, aircraft configuration information, and aircraft air data.
2. Description
A. The Engine fuel consists of:
- Distribution section (Ref. AMM D/O 73-10-00-00)
- Controlling section (Ref. AMM D/O 73-20-00-00)
- Indicating section (Ref. AMM D/O 73-30-00-00)